No CrossRef data available.
Article contents
The lifting two-dimensional aerofoil between slotted walls
Published online by Cambridge University Press: 09 April 2009
Summary
A mathematical theory is developed which enables the wind-tunnel corrections to the lift and moment forces acting on an aerofoil in subsonic two-dimensional flow to be calculated. The usual “averaged” boundary condition for slotted walls is assumed and the corrections obtained by successive approximation from the open-jet tunnel.
- Type
- Research Article
- Information
- Copyright
- Copyright © Australian Mathematical Society 1963